Experimental Flight Control Function for Electronic Flight Control System of High Aspect Ratio Light Utility Aircraft

机译：高纵横比光公用事业飞机电子飞行控制系统的实验飞行控制功能

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Aircraft technology demonstrator is an aircraft which is used for experimental and demonstration purpose. This type of aircraft has a unique capability, i.e. demonstrating the experimental or newly developed system. The consequence is the aircraft not only has to be able to ensure its own safety like a normal aircraft, but also needs to be capable to return the aircraft to safety in case of the experimental system. This article presents a design for Electronic Flight Control System to safely execute experimental Flight Control Laws in flight test. The purpose of this research is to provide a relatively safe way to test newly developed Flight Control Laws in experimental flight. This research uses linear models of the Light Surveillance Aircraft, which have been developed in LAPAN Indonesia since 2014. The simulations that have been done indicate that the Experimental System is able to execute the experimental commands and reduce accidental risk by giving a relatively safer signal whenever the aircraft is going into potentially dangerous maneuver.

机译：飞机技术示范器是一种用于实验和示范目的的飞机。这种类型的飞机具有独特的能力，即展示实验或新开发的系统。结果是飞机不仅必须能够确保其自身的安全性，如普通飞机，而且需要能够在实验系统的情况下能够将飞机返回到安全。本文介绍了电子飞行控制系统的设计，以安全地执行飞行试验中的实验飞行控制法。本研究的目的是提供一种相对安全的方法来测试实验飞行中的新开发的飞行控制法。本研究采用自2014年以来在莱山印度尼西亚开发的光监测飞机的线性模型。已经完成的模拟表明实验系统能够通过在每当时提供相对更安全的信号来执行实验命令并降低意外风险。飞机进入潜在的危险机动。

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《International Seminar on Aerospace Science and Technology》|2020年|1 volume (various pagings) :|共10页
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P. A. P. Suseno; S. Bahri;
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中图分类 V2-532;
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Electronic Flight Control System; High Aspect Ratio Light Utility Aircraft; used;

机译：电子飞行控制系统;高纵横比光公用事业飞机;使用;

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1. An alternative flight control system for an unmanned aircraft whose flight control system fails during a longitudinal flight with constant forward velocity [J] . Agneta M. BALINT, ?tefan BALINT INCAS Bulletin . 2010,第4期

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4. Experimental Flight Control Function for Electronic Flight Control System of High Aspect Ratio Light Utility Aircraft [C] . P. A. P. Suseno, S. Bahri International Seminar on Aerospace Science and Technology . 2020

机译：高纵横比光公用事业飞机电子飞行控制系统的实验飞行控制功能
5. Flight Mechanics and Flight Control for a Multibody Aircraft: Long-Endurance Operation at High Altitudes =Flugmechanik und Flugregelung von Mehrk?rperflugzeugen [D] . K?the, Alexander. 2019

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6. The control of tricarboxylate-cycle oxidations in blowfly flight muscle. The oxidized and reduced nicotinamide-adenine dinucleotide content of flight muscle and isolated mitochondria the adenosine triphosphate and adenosine diphosphate content of mitochondria and the energy status of the mitochondria during controlled respiration. [O] . R G Hansford 1975

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7. An alternative flight control system for an unmanned aircraft whose flight control system fails during a longitudinal flight with constant forward velocity [O] . Agneta M. BALINT, Ştefan BALINT 2010

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8. Design and Flight Test of the Propulsion Controlled Aircraft (PCA) Flight ControlSystem on the NASA F-15 Test Aircraft [R] . Wells, E. A., Urnes, J. M. 1994

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Experimental Flight Control Function for Electronic Flight Control System of High Aspect Ratio Light Utility Aircraft

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